BAE Systems Hawk T1
Overview
The BAE Systems Hawk T1 is a military aircraft manufactured by BAE Systems, with the profile centered on its trainer role. Its recorded introduction date is 1976. The current production-status field is listed as In Production. The listed crew requirement is 2. Power is provided by 2 Adour 1 engines. Recorded dimensions include length 37.4 ft, wingspan 32.6 ft, height 13.1 ft. Maximum takeoff weight is listed as 11244 lb. Listed performance includes maximum speed 648 kt, range 1,000 nautical miles, service ceiling Rolls-Royce (Turbomeca) ft. Its ICAO type designator is HAWK. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
Specifications
| ICAO Type Code | HAWK |
|---|---|
| Introduction Date | 1976 |
| Crew | 2 |
| Length | 37.4 ft |
| Wingspan / Rotor Diameter | 32.6 ft |
| Height | 13.1 ft |
| Max Takeoff Weight | 11244 lb |
| Max Speed | 648 kt |
| Range | 1,000 nm |
| Service Ceiling | Rolls-Royce (Turbomeca) |
| Engine Manufacturer | Adour |
| Engine Model | 1 |
| Engine Count | 2 |
Data verification status: Partially Verified